[Federal Register: May 7, 2004 (Volume 69, Number 89)]
[Rules and Regulations]
[Page 25488]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr07my04-5]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 2003-NE-46-AD; Amendment 39-13557; AD 2004-07-13]
RIN 2120-AA64
Airworthiness Directives; General Electric Company CF6-80C2
Series Turbofan Engines; Correction
AGENCY: Federal Aviation Administration, DOT.
ACTION: Final rule; correction.
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SUMMARY: This document makes a correction to Airworthiness Directive
(AD) 2004-07-13. That AD applies to General Electric Company (GE) CF6-
80C2 series turbofan engines. That AD was published in the Federal
Register on April 1, 2004 (69 FR 17033). The amendatory text in the
Applicability section is incorrect. This document corrects the aircraft
models that these engines are installed on. In all other respects, the
original document remains the same.
DATES: Effective Date: Effective April 1, 2004.
FOR FURTHER INFORMATION CONTACT: Karen Curtis, Aerospace Engineer,
Aircraft Certification Office, FAA, Engine and Propeller Directorate,
12 New England Executive Park, Burlington, MA 01803; telephone (781)
238-7192; fax (781) 238-7199.
SUPPLEMENTARY INFORMATION: A final rule AD, FR Doc. 04-7235, that
applies to General Electric Company (GE) CF6-80C2 series turbofan
engines was published in the Federal Register on April 1, 2004 (69 FR
17033). The following correction is needed:
Sec. 39.13 [Corrected]
0
On page 17034, in the first column, in the Amendatory Section,
Applicability paragraph (c), in the eighth line, ``A300 and A330'' is
corrected to read ``A300 and A310''.
Issued in Burlington, MA, on May 3, 2004.
Jay J. Pardee,
Manager, Engine and Propeller Directorate, Aircraft Certification
Service.
[FR Doc. 04-10429 Filed 5-6-04; 8:45 am]
BILLING CODE 4910-13-P